CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins in Supersonic Flow-Reference-Cited by-同舟云学术

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CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins in Supersonic Flow

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

DeSpirito James¹,Vaughn Milton²,Washington William²

Affiliation:

1. U.S. Army Research Laboratory

2. U.S. Army Aviation and Missile Command

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4509

Reference17 articles.

1. Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile

2. Experimental study of tail-span effects on a canard-controlled missile

3. a)

4. Technical Report RD-77-8, Redstone Arsenal, AL,

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